Status: In production. Number: 19 . Thrust: 999.60 kN (224,719 lbf). Specific impulse: 311 s. Specific impulse sea level: 245 s. Burn time: 300 s.
Chambers: 4. Oxidizer to Fuel Ratio: 2.39.
Country: Russia. Launch Vehicles: Soyuz-ST-B. Propellants: Lox/Kerosene. Stages: Soyuz ST-1. Agency: Glushko bureau. Bibliography: 318, 7498. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9RetroSearch is an open source project built by @garambo | Open a GitHub Issue
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